DELTA 1 R/B, 2661

Orbit data source: Space-Track

DELTA 1 R/B, 2661 is space debris in SSO originally from a launch on Thu, 26 Jan 1967 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
2661, 1967-006B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
1967-01-26 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DELTA 1 R/B
1 02661U 67006B   25255.94848089 -.00000042  00000-0  33887-4 0  9993
2 02661 101.9597 321.2849 0064644 239.6204 293.0999 12.68015237713016
Epoch: 2025-09-12T22:45Z
TLE epoch observation values (Epoch: 2025-09-12T22:45:48.748Z)
Latitude
7.72779°
Longitude
169.28187°
Altitude
1,372.528 km
Speed
7.182 km/s
True Right ascension
09h 31m 41s
True Declination
7° 41' 09"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
17:04:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,437.772 km
Perigee altitude
1,337.37 km
Semi-major axis
7,765.708 km
Eccentricity
0.00646
Inclination
101.9597°
RAAN
321.2849°
Arg. of periapsis
239.6204°
True anomaly
292.41638°
Mean anomaly
293.0999°
Eccentric anomaly
292.75835°
Mean motion
3.17155 °/min
Orbital period
113.51 mins
BSTAR
0.000033887
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Other satellites on launch #6 in the year 1967 (1967-01-26 UTC)

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